WO2013162131A1 - Turbine à réaction - Google Patents

Turbine à réaction Download PDF

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Publication number
WO2013162131A1
WO2013162131A1 PCT/KR2012/008151 KR2012008151W WO2013162131A1 WO 2013162131 A1 WO2013162131 A1 WO 2013162131A1 KR 2012008151 W KR2012008151 W KR 2012008151W WO 2013162131 A1 WO2013162131 A1 WO 2013162131A1
Authority
WO
WIPO (PCT)
Prior art keywords
hole
plate
guide plate
fluid
rotating
Prior art date
Application number
PCT/KR2012/008151
Other languages
English (en)
Korean (ko)
Inventor
이정석
Original Assignee
써클파워 주식회사
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 써클파워 주식회사 filed Critical 써클파워 주식회사
Publication of WO2013162131A1 publication Critical patent/WO2013162131A1/fr

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical

Definitions

  • the present invention relates to a jet turbine, and more particularly, it is possible to easily rotate the rotating plate using a low pressure fluid flowing in an oblique direction, and when the fluid flows into the rotating plate and when it flows out from the rotating plate
  • the present invention relates to a jet turbine which hardly causes a pressure drop.
  • a turbine converts energy of a fluid such as water, gas, and steam into useful mechanical energy, and the fluid collides with a plurality of blades fastened to a rotating shaft at high speed to be converted into rotating energy.
  • the turbine may be a steam turbine that emits steam from the nozzle and strikes the blade to rotate the turbine, a gas turbine that uses energy of high temperature and high pressure gas, and an air turbine that uses energy of high pressure compressed air.
  • the conventional turbine is suitable for large-scale power generation facilities, such as thermal power generation or nuclear power generation because the blade must be rotated using a high pressure fluid.
  • a large power plant has a problem in that the initial construction cost is high, and because a high-voltage electricity in one area to be transmitted to different areas, it is necessary to construct a plurality of transmission towers, the construction cost of the transmission tower and There is a problem that additionally incurs maintenance costs.
  • An object of the present invention for solving the problems of the prior art as described above is to provide a jet turbine that can generate a mechanical drive force even when using a low pressure fluid without using a blade.
  • Another object of the present invention is to provide a jet turbine that can be manufactured in a small size, it is possible to build a small power plant in a specific area requiring electricity.
  • Another object of the present invention is to provide a jet turbine that does not use a blade of a complex shape, the production cost is reduced, and the productivity is improved.
  • the present invention is a hollow housing and one side and the other side is open;
  • a rotating plate provided to rotate inside the housing and having a plurality of rotating guide holes formed along an edge thereof;
  • An inlet guide plate fixed to one side of the housing and having one or more inlet holes formed to allow fluid to flow into a position opposite to one end of the rotary induction hole;
  • An outlet guide plate which is fixed to the other side of the housing and has at least one outlet hole formed so that the fluid is discharged to a position opposite to the other end of the rotary induction hole;
  • a rotating shaft integrally passing through the rotating plate, the inflow guide plate, and the outflow guide plate, wherein the inflow hole includes a portion formed to be inclined in a direction in which the rotation plate rotates toward the rotation plate. It provides a jet turbine, characterized in that for rotating the rotating plate while the fluid flowing into the rotation guide side.
  • the inflow guide plate may include a first inflow guide plate and a second inflow guide plate in close contact with the outside of the first inflow guide plate, and the inflow hole may be disposed at a position opposite to the rotation guide hole of the first inflow guide plate.
  • a first inlet hole formed to be inclined in a direction in which the rotating plate rotates toward the rotating plate, and formed at a position opposite to the first inlet hole of the second inlet guide plate in a direction perpendicular to the second inlet guide plate. It provides a jet turbine comprising a second inlet hole is formed.
  • the outflow guide plate may include a first outflow guide plate fixed to the other side of the housing and a second outflow guide plate in close contact with the outside of the first outflow guide plate, and the outflow hole may be configured to rotate the first outflow guide plate. It provides a jet turbine, characterized in that it comprises a first outlet hole formed in a position facing the guide hole, and a second outlet hole formed in a position facing the first outlet hole of the second inlet guide plate.
  • the rotating plate may include a first rotating plate provided to rotate on one side of the housing, and a second rotating plate provided to rotate on the other side of the housing, wherein the rotating guide is formed along an edge of the first rotating plate.
  • the first rotating guide hole is formed in a direction perpendicular to the first rotating plate, and is formed at a position opposite to the first rotating guide hole along an edge of the second rotating plate, and the first rotating plate moves toward the outlet hole. It provides a jet turbine comprising a plurality of second rotary induction hole is formed to be inclined in a direction opposite to the rotation direction.
  • the side opposite to the direction in which the rotary plate of one end of the rotary induction hole facing the inlet hole is characterized in that it comprises a fluid guide portion formed in the form along the moving direction of the fluid flowing into the rotary induction hole in the inlet hole Provided is a jet turbine.
  • the plurality of the inlet hole provides a jet turbine, characterized in that configured in fewer than the plurality of rotary induction hole.
  • first coupling guide in a direction opposite to the edge of the first rotating plate or the edge of the first outflow guide plate of the edge of the inlet guide plate in which the inlet hole is formed or the edge of the second rotating plate in which the second rotation guide hole is formed.
  • a second coupling guide portion is formed so as to rotate along the first coupling guide portion at a position opposite to the first coupling guide portion of the edge of the first rotating plate or the edge of the outflow guide plate.
  • the jet turbine provides a jet turbine, characterized in that the plurality is arranged in a row, the outlet hole of one jet turbine adjacent to each other and the inlet hole of the other jet turbine is interconnected.
  • the diameter of the inlet hole located in each jet turbine provides a jet turbine, characterized in that configured to increase gradually along the direction in which the fluid is moved.
  • a plurality of the housings are arranged in a row along the rotation axis, the rotating plate is provided with a plurality so as to be rotated in each of the plurality of housings, the inlet guide plate is an outer body in the direction in which the fluid flows out of the plurality of housings It is fixed to the end of the housing which is located in the, the guide plate is fixed to the end of the housing which is located in the outer periphery in the direction of the fluid out of a plurality of the housing, is positioned to be fixed between the adjacent housings, adjacent to each other At least one fluid transfer plate is formed at a position opposite to the rotation induction hole of the rotating plate so that fluid is transferred, wherein the fluid transfer hole is in a direction in which the rotating plate rotates toward a direction in which the fluid is moved.
  • the jet turbine according to the present invention pressurizes the rotary plate in the rotation direction while the fluid flows into the rotary induction hole of the rotary plate in an oblique direction, so that the rotary plate can be easily rotated even when a low pressure fluid is used.
  • the jet turbine according to the present invention does not require a separate blade, and can be manufactured in a small size, and can generate a mechanical driving force by using the pressure of the fluid, and thus can produce a small amount of electricity required in the region. From the power source of the generator, there is an effect that can be widely used in the propeller drive source of the ship, the engine of the jet plane, automobiles, etc., and does not use a blade of a complex shape, the production cost is reduced, the productivity is improved.
  • the jet turbine according to the present invention has the effect of being able to reuse the fluid and increase the rotational efficiency by having a plurality of arranged side by side, or having a plurality of rotary plates.
  • FIG. 1 is a view schematically showing a jet turbine according to a preferred embodiment of the present invention.
  • FIG. 2 is an exploded view illustrating a jet turbine according to a preferred embodiment of the present invention.
  • FIG. 3 is a cross-sectional view taken along line AA ′ of FIG. 1.
  • FIG. 4 is a cross-sectional view taken along line BB ′ of FIG. 1.
  • 5 and 6 are views for explaining the fluid guide portion of the jet turbine according to an embodiment of the present invention.
  • FIG. 7 is a view illustrating a coupling guide of a jet turbine according to a preferred embodiment of the present invention.
  • FIG. 8 is a view illustrating an embodiment of a state where a plurality of jet turbines of the present invention are provided.
  • FIG 9 is a view illustrating another embodiment of the jet turbine of the present invention.
  • FIG. 1 is a view schematically showing a jet turbine according to a preferred embodiment of the present invention
  • Figure 2 is an exploded view showing a jet turbine according to a preferred embodiment of the present invention.
  • a jet turbine 5 includes a housing 10, a rotating plate, an inlet guide plate, an outlet guide plate, and a rotating shaft 50.
  • the housing 10 is formed in a cylindrical shape and has an empty space 12 therein.
  • One side and the other side of the housing 10 are configured to be open, and first and second fixing parts 14 and 16 are formed outwardly along one side and the other side of the circumference.
  • the rotating plate is formed in a disk shape and is provided to rotate in the space portion 12 of the housing 10, the first rotating plate 30 provided to rotate on one side of the housing 10, the housing 10 It includes a second rotating plate 35 provided to be rotated on the other side inside.
  • a plurality of first rotating guides 32 are formed in the first rotating plate 30 along the edge thereof, and a plurality of first rotating guides 32 are formed in the second rotating plate 35 opposite the first rotating guide holes 32 along the edge thereof.
  • the second rotary guide hole 37 is formed.
  • the first rotation guide 32 is formed in a direction perpendicular to the first rotation plate 30, the second rotation guide hole 37 toward the first outflow guide plate 40 to be described later toward the first rotation plate 30 It is formed to be inclined in a direction opposite to the direction of rotation.
  • the inclination angle of the second rotary induction hole 37 is composed of 25 ° to 50 °, preferably 45 °. Accordingly, the fluid that is moved from the first rotary guide hole 32 to the second rotary guide hole 37 presses the sidewall of the second rotary guide hole 37 along the inclined direction of the second rotary guide hole 37 while the second rotary plate is rotated. Will rotate (35). This will be described again with reference to the following drawings.
  • the inflow guide plate is fixed to an open side of the housing 10 and is formed to cover the open side of the housing 10, the edge of which is fixed to the first fixing part 14 of the housing 10.
  • 1 includes an inlet guide plate 20 and a second inlet guide plate 25 which is fixed in close contact with the outside of the first inlet guide plate 20.
  • the first inlet guide plate 20 and the second inlet guide plate 25 may be integrally formed with each other or may be separately formed and fixed to each other.
  • the first fixing part 14, the first inlet guide plate 20, and the second inlet guide plate 25 of the housing 10 may be firmly coupled to each other by using a coupling part such as a bolt, and the housing 10.
  • the first inflow guide plate 20 or the first inflow guide plate 20 and the second inflow guide plate 25 may be in close contact with each other.
  • a first inflow hole 22 is formed at a position facing the first rotation guide hole 32 of the first rotation plate 30 in the first inflow guide plate 20.
  • the first inflow guide plate 20 in order to allow the fluid introduced into the first inflow hole 22 of the first inflow guide plate 20 to easily flow into the first rotation induction hole 32 of the first rotation plate 30. It is preferable that the first inlet hole 22 is smaller in number than the first rotary induction hole 32 of the first rotating plate 30.
  • the first inflow hole 22 of the first inflow guide plate 20 is 25 ° to 50 °, preferably 30 ° in the direction in which the first rotation plate 30 rotates toward the first rotation plate 30. It is formed to be inclined. As such, the first inflow hole 22 of the first inflow guide plate 20 is formed to be inclined, and the first rotation induction hole 32 of the first rotation plate 30 is formed in the vertical direction, such that the first inflow hole 22 is formed.
  • the fluid flowing into the first rotary induction hole 32 obliquely along the inclined sidewall of the first rotary induction hole 32 rotates the first rotation induction hole 32 while pressing the sidewall of the first rotation induction hole 32.
  • At least one second inflow hole 27 is formed at a position facing the first inflow hole 22 in the second inflow guide plate 25.
  • the second inflow hole 27 is formed in a direction perpendicular to the second inflow guide plate 25, and two may be formed at one side and the other side of the outer surface of the second inflow guide plate 25.
  • the inflow guide groove 26 may be further concave along the inner edge facing the first inflow guide plate 20 in the second inflow guide plate 25.
  • the second inlet hole 27 is formed at least one along the outer edge of the second inlet guide plate 25, one end thereof penetrates the bottom surface of the inlet guide groove 26, the other end is the second inlet guide plate ( Penetrates the outside of 25).
  • an inlet pipe 28 is mounted at the other end of the second inlet hole 27 so that the fluid flowing from the inlet pipe 28 to the second inlet hole 27 is formed through a plurality of inlet guide grooves 26. 1 is easily guided to the inlet (22).
  • the outlet guide plate is fixed to the other open side of the housing 10, is formed to cover the other open side of the housing 10, the edge is fixed to the second fixing portion 16 of the housing 10 1 includes an outlet guide plate 40 and a second outlet guide plate 45 in close contact with and fixed to the outside of the first outlet guide plate 40.
  • the first and second outflow guide plates 40 and 45 are integrally formed with each other or separately formed and configured to be fixed to each other.
  • the second fixing part 16, the first outlet guide plate 40, and the second outlet guide plate 45 of the housing 10 may be firmly coupled to each other by using a coupling part such as a bolt, and the housing 10.
  • the first outflow guide plate 40 or the first outflow guide plate 40 and the second outflow guide plate 45 may be in close contact with each other.
  • first outflow guide plate 40 and the second outflow guide plate 45 may be integrally formed with each other or separately formed, and then may be closely fixed.
  • first outflow guide plate 40 may be omitted in some cases, in this case, the second outflow guide plate 45 is fixed to the second fixing portion 16 of the housing 10.
  • a first outlet hole 42 is formed at a position facing the second rotation guide hole 37 of the second rotating plate 35 in the first outlet guide plate 40.
  • the first outlet hole 42 is formed in a direction perpendicular to the first outlet guide plate 40.
  • a second outlet hole 47 is formed at a position facing the first outlet hole 42 in the second outlet guide plate 45, and the second outlet hole 47 is perpendicular to the second outlet guide plate 45. Is formed.
  • the fluid flowing into the first and second rotary guide holes 32 and 37 of the first and second rotary plates 30 and 35 flows out through the first and second outlet holes 42 and 47.
  • the first inflow hole 22 or the second inflow hole 27 or the first rotation induction hole 32 or the second rotation induction hole 37 or the first outflow hole 42 or the second outflow hole 47 The cross section may consist of a circular or polygonal or oval shape.
  • an outflow guide groove 46 may be further concave along the inner edge facing the first outflow guide plate 40 in the second outflow guide plate 45.
  • the second outlet hole 47 is formed at least one along the outer edge of the second outlet guide plate 45, one end of which penetrates the bottom surface of the outlet guide groove 46, and the other end thereof has the second outlet guide plate ( Penetrates the outside of 45).
  • an outlet pipe 48 is mounted at the other end of the second outlet hole 47 so that the fluid flowing out of the first outlet hole 42 is easily transferred to the second outlet hole 47 through the outlet guide groove 46. The fluid guided to the second outlet hole 47 is easily discharged to the outside through the outlet pipe 48.
  • the rotating shaft 50 integrally penetrates the centers of the first and second inflow guide plates 20 and 25, the first and second rotation plates 30 and 35, and the first and second outflow guide plates 40 and 45. , 2 serves as the axis when the rotating plate (30, 35) is rotated.
  • the first and second rotating plates 30 and 35 are connected to the rotating shaft 50, and when the first and second rotating plates 30 and 35 are rotated, the rotating shaft 50 is also rotated to generate rotational energy.
  • Or between the first and second outflow guide plates 40 and 45 and the rotating shaft 50 may be watertight.
  • FIG. 3 is a cross-sectional view taken along line AA ′ of FIG. 1
  • FIG. 4 is a cross-sectional view taken along line B-B ′ of FIG. 1.
  • the external fluid guided to the second inlet hole 27 of the second inlet guide plate 25 is moved along the first inlet hole 22 of the first inlet guide plate 20.
  • the direction of movement of the first rotating plate 30 is obliquely bent.
  • the fluid moved from the first inlet hole 22 to the first rotary induction hole 32 of the first rotating plate 30 in this bent state is introduced into the first rotation induction hole 32 so that the kinetic energy of the fluid is rotated first.
  • the side wall of the guide hole 32 is pressed to rotate the first rotating plate 30.
  • the number of the first rotary guide holes 32 of the first rotating plate 30 should be larger than the number of the first inlet holes 22 of the first inlet guide plate 20, so that the first inlet hole 22 may be introduced.
  • the fluid can be smoothly moved to the first rotary induction hole (32).
  • the fluid pressurizing the side of the first rotating guide hole 32 is moved in the direction of the second rotating plate 35 and flows into the second rotating guide hole 37 of the second rotating plate 35.
  • the second rotary induction hole 37 is formed to be inclined in a direction opposite to the direction in which the first rotation plate 30 is rotated toward the first outflow guide plate 40, the fluid flowing into the second rotation induction hole 37
  • the fluid passing through the second rotation guide hole 37 of the second rotating plate 35 may include the first outlet hole 42 of the first outlet guide plate 40 and the second outlet hole of the second outlet guide plate 45. It is discharged to the outside through 47).
  • the first inflow hole 22 of the first inflow guide plate 20 is the second of the first rotation guide hole 32 and the second rotation plate 35 of the first rotation plate 30. It may be configured to have a smaller diameter than the rotary induction hole 37. Accordingly, when the fluid flows into the first and second rotary guide holes 32 and 37 from the first inlet hole 22, the pressure drop hardly occurs, so that the first and second rotary plates (low pressure) are used. 32, 35) there is an effect that can be easily rotated.
  • the jet turbine 5 of the present invention uses the first and second inlet guide plates 20 and 25. , Most of the fluid that is moved to the first rotating plate 30 through the second inlet hole 22, 27 is introduced into the first rotating guide hole 32 of the first rotating plate 30 without loss, and thus, the first rotating plate 32. ) Is pressed in the rotational direction. Accordingly, the first rotating plate 30 can be easily rotated even when a low pressure fluid is used without using a high pressure as in the prior art, and since the fluid does not press the blade, vibration and noise are not generated, There is no effect of damage caused by the repair cost is reduced.
  • 5 and 6 are views for explaining the fluid guide portion of the jet turbine according to an embodiment of the present invention.
  • FIG. 5 is a view illustrating the first rotating plate 30 on which the fluid guide part 33 is not formed.
  • a fluid moving at an angle of about 25 ° to 50 ° is introduced into the first rotating guide hole 32 of the first rotating plate 30.
  • the kinetic energy of the fluid presses the first side portion 32a provided in the direction in which the first rotating plate 30 rotates in the first rotating guide hole 32, thereby rotating the first rotating plate 30.
  • the fluid that is obliquely moved along the first inlet hole 22 of the first inlet guide plate 20 is a second position facing the first side portion 32a in the first rotary guide hole 32 according to the position thereof.
  • the end of the side portion 32b is also hit.
  • the fluid striking the end of the second side portion 32b is not guided in the direction of the first side portion 32a of the first rotary induction hole 32 and bounces out of the first rotation induction hole 32, thereby causing a normal flow of the fluid. It acts as a factor that hinders, eventually reducing the efficiency of the rotational energy of the first rotating plate (30).
  • FIG. 6 is a view illustrating the first rotating plate 30 on which the fluid guide part 33 is formed.
  • the first inlet hole 22 of the first inlet guide plate 20 is obliquely.
  • the moving fluid flows into the first rotary induction hole 32 of the first rotary plate 30.
  • the end of the second side portion 32b of the first rotary induction hole 32 is inclined at about 25 ° to 50 ° along the moving direction of the fluid flowing from the first inlet hole 22 to the first rotation induction hole 32.
  • the fluid guide part 33 is inserted into the fluid guide part 33 so that the fluid flowing in the direction of the second side part 32b of the first rotary induction hole 32 is easily directed in the direction of the first side part 32a of the first rotary induction hole 32. Is induced.
  • the kinetic energy of the fluid acting on the first side portion 32a of the first rotary induction hole 32 increases, so that the rotational energy efficiency of the first rotary plate 30 becomes higher.
  • FIG. 7 is a view illustrating a coupling guide of a jet turbine according to a preferred embodiment of the present invention.
  • the first rotation plate At the edge of the first inflow guide plate 20 in which the first inflow hole 22 is formed and the edge of the second rotation plate 35 in which the second rotation guide hole 37 is formed, the first rotation plate ( The first coupling guides 23 and 43 are protruded in a circular direction in a direction opposite to the edge of the frame 30 and the first outflow guide plate 40, and the edge of the first rotating plate 30 and the first outflow guide plate 30.
  • the second coupling guides 34 and 38 are concave so that the first coupling guides 23 and 43 are inserted and slidably rotated at positions opposite to the first coupling guides 23 and 43 at the edge of the 40. Is formed.
  • first rotating plate 30 and the second rotating plate 35 When the first rotating plate 30 and the second rotating plate 35 are rotated, the first coupling guides 23 and 43 and the second coupling guides 34 and 38 are slidably rotated to each other to form the first rotating plate ( 30 and the second rotating plate 35 may be configured to rotate more stably.
  • FIG. 8 is a view illustrating an embodiment of a state where a plurality of jet turbines of the present invention are provided.
  • the present invention includes a plurality of jet turbines 5, and the fluid discharged from the second outlet hole 47 of one jet turbine 5 adjacent to each other is used as the second jet turbine 5.
  • Inflow to the inlet 27 is configured to reuse the fluid.
  • a plurality of jet turbines 5 are arranged in a row, and the second outlet hole 47 of the one jet turbine 5 adjacent to each other and the second inlet hole 27 of the other jet turbine 5 closely adhere to each other.
  • the rotating shaft 50 may be provided in each of the plurality of jet turbine 5, or one may be provided integrally.
  • the fluid passing through the one jet turbine 5 is not discharged to the outside, but flows back to the other jet turbine 5, so that the fluid can be reused. There is an effect that can increase the efficiency.
  • FIG 9 is a view illustrating another embodiment of the jet turbine of the present invention.
  • the jet turbine 5 ′ of the present invention may include a plurality of first rotating plates 30 and second rotating plates 35.
  • a plurality of housings 10 are arranged in a line along the rotation shaft 50, and the rotating plate, that is, the first rotating plate 30 and the second rotating plate 35, are rotated inside each housing 10.
  • the first inlet guide plate 20 is fixed to the end of the housing 10 which is located outside the body in the direction of the fluid flow of the plurality of the housing 10
  • the second inlet guide plate 25 is the first inlet guide plate Are positioned integrally or mutually fixed on the outside of the 20.
  • the discharge guide plate is fixed to the end of the housing 10 which is located outside the body in the direction in which the fluid out of the plurality of the housing (10).
  • the outflow guide plate includes a first outflow guide plate 40 (shown in FIG. 3) and a second outflow guide plate 45. In some cases, the outflow guide plate 40 may be omitted.
  • the fluid transfer plate 39 is positioned between the housings 10 adjacent to each other.
  • the fluid transfer plate 39 includes a plurality of fluid transfer holes such that fluid is transferred to a position opposite to the first and second rotation guide holes 32 and 37 of the first and second rotary plates 30 and 35 adjacent to each other. 39a) is formed.
  • the fluid transfer hole 39a is formed to be inclined in a direction in which the first rotating plate 30 or the second rotating plate 35 rotates toward the direction in which the fluid moves.
  • the fluid discharged from the second rotary guide hole 37 of the second rotary plate 35 disposed in one housing 10 of the housing 10 adjacent to each other passes through the fluid transfer hole 39a and the other housing 10.
  • the first rotation of the first rotating plate 30 The side wall of the induction hole 32 is pressed to rotate the first rotating plate 30.
  • the first rotary plate 30 is rotated by the fluid flowing into the first rotary guide hole 32 of the first rotary plate 30 obliquely along the first inlet hole 22 of the first inlet guide plate 20 or Alternatively, it may be rotated by the fluid flowing obliquely into the first rotary guide hole 32 of the first rotating plate 30 along the fluid transfer hole 39a of the fluid transfer plate 39.
  • the fluid passing through the first rotating plate 30 presses the sidewall of the second rotating guide hole 37 along the inclined direction of the second rotating guide hole 37 so that the second rotating plate 35 is easily rotated. It is composed.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Hydraulic Turbines (AREA)

Abstract

La présente invention concerne une turbine à réaction capable d'entraîner en rotation une plaque rotative au moyen d'un fluide, le fluide s'écoulant de manière oblique dans un trou de guidage de rotation de la plaque rotative de façon à presser la plaque rotative dans une direction de rotation, en entraînant ainsi facilement la plaque rotative au moyen du fluide sous basse pression. En outre, la turbine à réaction de la présente invention élimine le besoin d'une ailette distincte et, par conséquent, peut être fabriqué avec une petite taille. La turbine à réaction selon la présente invention peut générer une force d'entraînement mécanique au moyen de la pression du fluide et, par conséquent, peut être largement utilisée dans la source d'énergie d'un petit générateur permettant de générer une petite quantité d'énergie électrique nécessaire à une zone spécifique, dans une source d'entraînement d'un propulseur d'un navire, dans un moteur à réaction d'un aéronef, dans un véhicule électrique, etc.
PCT/KR2012/008151 2012-04-26 2012-10-09 Turbine à réaction WO2013162131A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR1020120044049A KR101272820B1 (ko) 2012-04-26 2012-04-26 제트 터빈
KR10-2012-0044049 2012-04-26

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WO2013162131A1 true WO2013162131A1 (fr) 2013-10-31

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KR102217382B1 (ko) * 2018-12-18 2021-02-19 김희근 다단 증기터빈

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100550366B1 (ko) * 2004-03-17 2006-02-13 이재본 축류형 다단터빈
KR20070092841A (ko) * 2006-03-09 2007-09-14 피티엘중공업 주식회사 하이브리드 시너지 제트터빈 발전 시스템
KR20100105103A (ko) * 2009-03-20 2010-09-29 최혁선 축류형 다단터빈
WO2012030052A2 (fr) * 2010-08-31 2012-03-08 주식회사 에이치케이터빈 Turbine à réaction

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100550366B1 (ko) * 2004-03-17 2006-02-13 이재본 축류형 다단터빈
KR20070092841A (ko) * 2006-03-09 2007-09-14 피티엘중공업 주식회사 하이브리드 시너지 제트터빈 발전 시스템
KR20100105103A (ko) * 2009-03-20 2010-09-29 최혁선 축류형 다단터빈
WO2012030052A2 (fr) * 2010-08-31 2012-03-08 주식회사 에이치케이터빈 Turbine à réaction

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